LEADER 01781nam  2200469I  450 
001 9910706248103321
005 20171018095708.0
035   $a(CKB)5470000002455957
035   $a(OCoLC)1006643793
035   $a(EXLCZ)995470000002455957
100   $a20171018j201707    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aLow-Reynolds number aerodynamics of an 8.9 percent scale semispan swept wing for assessment of icing effects /$fAndy P. Broeren [and three others]
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dJuly 2017.
215   $a1 online resource (39 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2017-219533
300   $a"July 2017."
300   $a"Prepared for the 9th AIAA Atmospheric and Space Environments Conference sponsored by AIAA, Denver, Colorado, June 5-9, 2017."
300   $a"AIAA-2017-4372."
320   $aIncludes bibliographical references (pages 38-39).
606   $aAerodynamic configurations$2nasat
606   $aAircraft icing$2nasat
606   $aComputational fluid dynamics$2nasat
606   $aLeading edges$2nasat
606   $aSwept wings$2nasat
615  7$aAerodynamic configurations.
615  7$aAircraft icing.
615  7$aComputational fluid dynamics.
615  7$aLeading edges.
615  7$aSwept wings.
700   $aBroeren$b Andy P.$01386216
712 02$aNASA Glenn Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910706248103321
996   $aLow-Reynolds number aerodynamics of an 8.9 percent scale semispan swept wing for assessment of icing effects$93514422
997   $aUNINA